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NASA Technical Reports Server (NTRS) 19860015193: ALESEP. Part 2: A computer program for the analysis of leading edge separation bubbles on infinite swept wingsA program called ALESEP is presented for the analysis of the inviscid-viscous interaction which occurs due to the presence of a closed laminar-transitional separation bubble on an airfoil or infinite swept wing. The ALESEP code provides an iterative solution of the boundary layer equations expressed in an inverse formulation coupled to a Cauchy int